Non-ignition Evaluation Method for Hypergolic Propellant Using Microreactor

Author:

Lee Kyounghwan,Park Seonghyeon,Kang Hongjae,Lee Jongkwang

Funder

Hanbat National University

Publisher

The Korean Society of Propulsion Engineers

Subject

General Medicine

Reference13 articles.

1. Kang, H.J. and Kown, S.J., “Foundational Study and Performance Evaluation of Non-Toxic Hypergolic Propellants,“ The Korean Society for Aeronautical & Space Sciences, Jeju, Korea, pp. 268-271, 2013.

2. Numerical Study of Chemical Reaction for Liquid Rocket Propellant Using Equilibrium Constant

3. Lee, K.H., Park, S.H., Kang, H.J. and Lee, J.K., “Pre-Evaluation Method of Hypergolic Propellants Using Micro Reactors,” 56th KSPE Spring Conference, Jeju, Korea, pp. 77-80, May 2021.

4. A Review of the Technical Development on Green Hypergolic Propellant

5. Development of Reduced Toxicity Hypergolic Propellants

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